Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.
ICI Case No. QM 34939
- 1 2~
SILICON CARBIDE_FIBRE AND PROD~CTION THEREOF
This invention relates to silicon carbide fibres
and to a process for the production of the fibres.
Fibres of silicon carbide have in recent years
been used in an increasing variety of applications. Such
fibres have high heat resistance and they may have
high tensile strength and substantial flexibility. The
fibres may be used as such or they may be woven into the
form of a fabric before use. Applications of silicon
carbide fibres which have been proposed include many
reinforcement applications, such as in the reinforcement
of monolithic silicon carbide structures and of
structures made of other refractory materials in order
to produce structures of high strength and high fracture
toughness, particularly at elevated temperatures.
Silicon carbide fibres have also been proposed fGr use
in the reinforcement of metallic structures. Silicon
carbide fibres may also be used to reinforce organic
plastics materials, although in this application the
high heat resistance properties of the fibres are not as
relevant as in those applications in which metallic and
refractory materials are reinforced.
Various processes have been proposed for the
production of silicon carbide fibres.
Silicon carbide fibres have been produced by
thermal decomposition of organisilicon polymer
precursors in fibrous form. Thus, a solution of an
organosilicon polymer, a polycarbosilane, may be spun
into the form of a fibre and the fibre heated in an
inert atmosphere to remove the solvent from the fibre,
and the fibre may be heated at an even higher
temperature in order to pyrolyse the organosilicon
polymer and produce silicon carbide in fibrous form.
Organosilicon polymers which have been proposed for use
2r~3c~22~
-- 2
as precursors include those obtained from
dodecamethlcyclohexasilane formed by dechlorination of
CH3SiC13 with lithium (Yajima et al Chemical Letters
1975 pp 931 to 934 and 551 to 554), and from
polydimethylsilane by dechlorination with sodium (Chem.
Abst. 89, 130854).
Silicon carbide fibres may also be produced from
fibres of carbon. For example, in GB Patent 998089 there
is described a process for the production of fibres of
thè carbides of silicon, tantalum, molybdenum or
tungsten which comprises forming a cloth or group of
fibres of carbon and converting the cloth or group of
fibres in situ to fibres of the carbide by heating the
cloth or group of fibres in an inert atmosphere or in
vacuum in the presence of the chosen metal. For example,
a carbon cloth may be embedded in silicon powder and
heated to a temperature just below the melting point of
silicon.
Silicon carbide fibres may also be produced by a
chemical vapour deposition process in which a heated
core in the form of a fibre, eg a carbon fibre or a
tungsten wire, is drawn through a deposition chamber
into which a vaporised silicon containing reactant is
introduced and in which the reactant is decomposed
leading to deposition of silicon carbide onto the
fibrous core. The fibre which is produced has a
composite structure and does not consist entirely, or
even substantially of silicon carbide. For example, US
Patent 3433725 describes such a process in which the
reactant is silicon tetrachloride which decomposes and
reacts with carbon in fibrous form to produce a
composite fibre having a sheath of silicon carbide and a
core of carbon.
Yet a further process which has been proposed for
the production of silicon carbide fibres is to heat a
2~Z~
viscose rayon fibre wlth silicon, eg with silicon in the
form of colloidal silica, at elevated temperature (Chem
Abst 102, 97733).
Silicon carbide fibres made by the aforementioned
processes suffer from a disadvantage in that, although
monolithic sintered silicon carbide structures may be
able to withstand prolonged exposure to elevated
temperatures of the order of 1500C with little or no
loss in strength of the structures, silicon carbide
fibres produced by many of the processes which have been
described hitherto suffer a substantial loss in strength
on exposure to such an elevated temperature, and even on
exposure to lower temperatures of the order of lOOO~C,
with the result that at such elevated temperatures there
is a corresponding decrease in the reinforcing effect
produced by the silicon carbide fibres in the matrix in
which the fibres are incorporated. This instability and
loss of strength of silicon carbide fibres may occur not
only when the fibres are heated in an oxygen-containing
atmosphere, eg in air, at such elevated temperatures but
also when the fibres are heated to such temperatures
in an inert atmosphere.
The adverse effect of elevated temperatures on
the strength of silicon carbide fibres is well
documented. For example, in Proc. Conf. on Advances in
Composite Materials, (ICCM-III) Paris, 1980, 2 page 17
it is reported that SiC yarn fibres suffer significant
losses in room temperature strength after heating at or
above 1200C and that commercial fibres exhibit a drop
in strength when heated above about lOOO~C. In Ceram.
Eng. Sci. Prog. 7 pages 901 to 903, 1986 it is reported
that 'Nicalon' silicon carbide fibres produced by
pyrolysis of an organosilicon polymer in fibrous form
suffer significant losses in mechanical properties when
the fibres are contacted with hot gaseous environments
2g~ 2~
or hot liquids, and in Ceram. ~ng. Sci. Prog. 7 pages
914 to 930, 1986 it is reported that 'Nicalon' silicon
carbide fibres suffer a major loss in tensile strength
when heated in argon at 1400C. Silicon carbide fibres
produced by chemical vapour deposition onto a suitable
fibrous core also suffer a loss in strength when heated
to elevated temperatures. Thus, Proc. Int. Conf. on
SiC, Miami, Univ. of South Carolina Press, ed. R.C.
Marshall, 1973, pages 386 to 393 reports that silicon
carbide fibres produced by thermal decomposition of
methyltrichlorosilane on a tungsten core suffered
substantial loss in rupture strength even when heated to
a temperature as low as 1000C, and a very substantial
loss when heated to a temperature above 1200C, and a
similar loss in strength of a silicon carbide fibre
produced by chemical vapour deposition on a carbon core
was reported in J Composite Materials, 9 1975 pages 73
to 76.
It is believed, without prejudice, that this
instability and loss of strength of silicon carbide
fibres at elevated temperatures is associated with the
composition of the fibres. For example, fibres which
comprise a sheath of silicon carbide on a core of a
different material, eg of carbon or of tungsten, are
believed to suffer a loss of strength at elevated
temperatures as a result of reaction between the silicon
carbide sheath and the material of the core. Fibres
produced by decomposition of a polymer precursor in
fibrous form may comprise unreacted silica or unreacted
carbon the presence of which may lead to reaction and to
a decrease in the strength of the fibre at elevated
temperatures. The excess of silica or carbon which may
be present in such a fibre may also react at elevated
temperatures with the matrix in which the silicon
2~
carbide fibre is incorporated with possible deleterious
consequences.
The present invention relates to silicon carbide
fibres, and to a process for the production of the
fibres, the fibres when heated at elevated temperature
eg to a temperature of the order of 1200C to 1500C,
suffering a loss in strength, if any, which is not as
great as that suffered by silicon carbide fibres
produced by processes which have generally been
described hitherto.
Furthermore, the silicon carbide fibres of the
present invention have a microstructural stability when
heated to elevated temperatures which is superior to
that of silicon carbide fibres produced hitherto.
According to the present invention there is
provided a process for the production of a
silicon carbide fibre which comprises forming a fibre
from a homogeneous mixture comprising particulate
silicon carbide dispersed in a solution of an organic
polymeric material in a liquid medium, and heating the
fibre at elevated temperature in order to decompose the
organic polymeric material and to sinter the particles
of silicon carbide.
The silicon carbide fibre produced by the
aforementioned process has a structure which is
distinguished from that of fibres described hitherto,
and in a further embodiment of the invention there is
provided a fibre of silicon carbide in which the silicon
carbide constitutes greater than 9G% by weight of the
fibre and in which the fibre is substantially
homogeneous across a transverse section of the fibre.
The silicon carbide fibre of the invention of
substantially homogeneous across a transverse section of
the fibre, that is it has a substantially uniform
composition across this transverse section, unlike
Z~ 2~
silicon carbide fibres which comprise a sheath of
silicon carbide on a core of a different material which
clearly are not homogeneous across a transverse section
of the fibre. Furthermore, as silicon carbide fibres
produced by pyrolysis of a polymer precursor therefor
generally contain substantial proportions of oxygen,
present as silica, and possibly of carbon, these latter
fibres generally comprise less than 90% by weight of
silicon carbide and also are not homogenous, and are
thus distinguished from the fibres of the present
invention.
It is to be understood that the present invention
does not exclude silicon carbide fibres which are
substantially homogeneous across a transverse section of
the fibre but which have a surface layer of a material
other than silicon carbide which may be present in order
to modify the interfacial strength between the fibre and
a susbtrate in which the fibre is incorporated.
The silicon carbide fibre of the invention has a high
degree of crystallinity and is polycrystalline, and the
invention also provides a silicon carbide fibre which is
polycrystalline, by which we mean that the fibre
comprises a plurality of separate crystallites of mean
size greater than 500A, as measured by X-ray
diffraction. This is in contrast to the known silicon
carbide whiskers which, although they have a high degree
of crystallinity, comprise a single crystal of silicon
carbide in fibrous form. Such whiskers, which can be
produced by growing a single crystal, have somewhat
limited dimensions when compared with fibres which can
be made by the process of the present invention.
In contrast to the crystalline nature of the
fibres of the invention the fibres produced by thermal
decomposition of precursors in fibrous form and by
chemical vapour deposition tend to comprise substantial
2~ Z~
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proportions of amorphous or partiallY crystalline
material and to have a small mean crystallite size.
The highly crystalline nature of the fibre of the
invention provides an additional benefit in that, in
contrast to such known fibres, there is little change in
crystallinity of the fibre on heating to elevated
temperatures and little change in the size of the
crystallites of silicon carbide in the fibres, and thus
little if any phase change on heating to elevated
temperatures. The fibres of the invention may thus be
defined in yet a further way. Thus, the silicon carbide
fibres of the invention, when heated at an elevated
temperature of 1500C or greater for a prolonged period
of time, eg for 10 hours or more, show little or no
increase in crystallinity or change in mean crystallite
size.
The fibre of the invention which is defined as
being polycrystalline and as having a mean crystallite
size of greater than 500A, as measured by X-ray
diffraction, is itself not necessarily substantially
homogeneous over a transverse section of the fibre,
although it preferably is substantially homogeneous.
Thus, the silicon carbide fibre which is polycrystalline
and has a mean crystallite size of greater than 500A may
comprise a sheath of silicon carbide on a core of
another material, preferably a material which is
resistant to degradation at elevated temperatures and
which does not react with the silicon carbide at
elevated temperatures. Such a fibre may be produced by
depositing onto a core of another material a sheath of a
homogeneous mixture comprising particulate silicon
carbide dispersed in an aqueous solution of an organic
polymeric material in a liquid medium, and heating the
fibre at elevated temperature in order to decompose the
z~
organic polymeric material and to sinter the particles
of silicon carbide.
The fibre production process of the invention is
effected with silicon carbide in particulate form which,
ln contrast to known production processes, is formed
before the stage at which the fibre itself is produced.
Thus, in the process it is possible to effect the fibre
production process with relatively pure uncontaminated
silicon carbide with the result that the disadvantages
of fibres containing smaller or larger amounts of
impurities, eg silica and/or carbon, and produced by
known processes in which a precursor in fibrous form is
chemically decomposed, are overcome.
In order to produce relatively pure silicon
carbide for conversion to fibrous forms the method by
which the silicon carbide particles are produced is
clearly of some importance. Several methods are known by
which particulate silicon carbide may be produced. For
example, particles of silicon carbide have traditionally
been produced by the so-called carbothermic reaction in
which an intimate mixture of carbon and silica is heated
in an inert atmosphere to produce the carbide according
to the equation
SiO 2 + 3C - SiC + 2CO.
However, although in the process the required
stoichiometric proportion of silica to carbon may
readily be achieved, that is, three moles of carbon for
every mole of silica, it may be difficult to achieve the
necessary intimate contact between the carbon and the
silica in order that a product of uniform composition
may be produced, that is a uniform composition on a
molecular scale. In particular, the particles which are
produced, which are nominally silicon carbide, may be
contaminated with unreacted silica and/or carbon. This
may be the case even when very small particles of silica
2~i~3(~2:~
g
and carbon are used, for example silica sol and carbon
black. Furthermore, in this traditional process it may
also be difficult to produce particle of silicon carbide
having a very small size, eg a size of less than
S 1 micron.
In an alternative process particles of silicon
carbide may be produced by pyrolysis of rice hulls, as
described in Thermochimica Acta, 81, (1984) 77-86.
Rice hulls consist of silica and cellulose, which
yields a mixture of silica and carbon when thermally
decomposed. Rice hulls have a very high surface area and
this, together with the intimate contact between the
carbon and silica in the thermally decomposed rice
hulls, enables silicon carbide to be formed by
subsequent pyrolysis at relatively low temperatures.
However, the molar ratio of silica to carbon in the
thermally decomposed rice hulls is generally about 1 ~o
4.7, that is there is a substantial excess of carbon
over the stoichiometrically required proporticn of 1:3.
A preferred process for the production of
particles of silicon carbide which are of high purity,
which contain little if any unreacted silica and/or
carbon, and which are particularly suitable for use in
the production of the silicon carbide fibres of the
present invention are those produced by the process of
European Patent Application 0 239 301A in which there is
described a process for the production of a silicon
carbide which comprises producing an oxygen-containing
polymeric product by reacting a first reactant which
comprises at least one compound of silicon having two or
more groups reactive with hydroxyl groups with a second
reactant which comprises at least one organic compound
have two or more hydroxyl groups, heating the polymeric
product in an inert atmosphere to produce a coked
product containing carbon and silica, and heating the
2~
-- 10 --
coked product to effect a carbothermic reaction between
the silica and the carbon, in which the proportion of
the first and second reactants ls chosen such that in
the coked product the proportion by weight of carbon to
the silica is close to the proportion which is
theoretically required to produce the silicon carbide.
The disclosure of the aforementioned European
Patent Application is incorporated herein by reference.
The particles of silicon carbide in the
composition from which the fibres of the invention are
produced may be of substantially the same particle size
or they may comprise a plurality of particle sizes.
Indeed the latter is preferred as the use of a plurality
of particle sizes assists in the production of a high
density silicon carbide fibre. The sizes of the
particles of silicon carbide will be determined at least
to some extent by the diameter of the fibre which is to
be produced in the process of the invention as the
maximum dimension of the particles should be less than,
and preferably substantially less than, the diameter of
the fibre which is to be produced. It is preferred that
the maximum dimension of the particles of silicon
carbide is not greater than 50 microns, more preferably
not greater than 10 microns, although it is of course
possible for particles having a maximum dimension
greater than 50, or 10 microns to be used in the
process. In general, the maximum dimensions of the
particles will be in the range 0.1 to 5 microns. For
reasons which have been explained previously the
particles of silicon carbide should be of high purity,
and it is preferred that the particles of silicon
carbide used in the process of the invention should
comprise at least 90% by weight of silicon carbide. In
order to produce fibres of silicon carbide which are of
high strength and which retain their high strength on
2~ 2~
-- 11 --
prolonged exposure to elevated temperature it is
preferred that the silicon carbide used ln ~he process
of the invention comprises at least 95% by weight
silicion carbide, and thus that the silicon carbide in
the fibre of the invention constitutes at least 95% by
weight of the fibre.
The particles of silicon carbide preferably have
a low aspect ratio as this aids the fibre production
process. A maximum aspect ratio of 2 is preferred.
Substantially spherical particles are most preferred.
The composition from which the fibres are
produced comprises a solution of an organic polymeric
material in a liquid medium. Although it is possible for
the liquid medium to be an organic material it is much
preferred, for reasons of low toxicity and flammability,
that the liquid medium is an aqueous medium. In general
the liquid medium will be water.
The composition from which the fibres are
produced may comprise any organic polymeric material
which is soluble in the li~uid medium.
Suitable water-soluble organic polymeric
materials include, for example, cellulose derivatives,
e.g hydroxy propyl methyl cellulose, polyacry~~amide,
polyethylene oxide, and polyvinyl pyrollidone. A
preferred organic polymeric material, which is
particularly suitable for use in production of fibres,
is a hydrolysed polymer or copolymer of vinyl ester,
particularly a hydrolysed polymer or copolymer of
vinyl acetate. The degree of hydrolysis of the polymer
or copolymer of vinyl acetate is preferably at least
50%, more preferably in the range 70% to 90%,
particularly where the composition is to be processed at
or near ambient temperature.
The concentration of the organic polymeric
material in the liquid medium will depend on a number of
za~ &~2~ '
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factors, for example, the nature of the organic
polymeric material, the size and size distribution of
the particulate silicon carbide and its mean apsect
ratio, and on the relative proportions by volume of the
silicon carbide, of the liquid medium, and of the
organic polymeric material. A concentration of organic
polymeric material in the liquid medium in the range 5%
to 60% by volume will generally suffice.
It is preferred that in the composition from
which the fibres are produced the concentration of
particulate silicon carbide is reasonably high as the
lower is the proportion of silicon carbide the greater
is the proportion of organic polymeric material and of
liquid medium which must be removed from the fibre in
the later stages of the process, although the
proportion of silicon carbide particles which is used
is dependent in part on the method by which the fibre is
produced, as will be discussed hereafter. It is
preferred that the proportion of silicon carbide in the
composition is as high as possible consistent with the
composition retaining its ability to be converted into a
fibrous form in the process although the proportion of
silicon carbide paticles which is used is dependent in
part on the method by which the fibre is produced, as
will be discussed hereafter. It is thus preferred that
the compositon comprises at least 50% by volume of
particulate silicon carbide. The composition may
comprise at least 60% by volume of silicon carbide, or
even as much as 70% or more by volume of silicon
carbide.
The composition from which the fibre is produced
comprises a homogeneous mixture of the components of the
composition, that is a composition in which the
particles of silicon carbide are homogeneously
distributed throughout the composition. The mixing of
25)(~ 21
- 13 -
the components of the composition is preferably effected
under conditions of high shear in order to ensure
homogeneity in the composition. For example, where the
composition is in the form of a highly viscous dough the
mixing of the composition may be effected in a screw
extruder or on a twin-roll mill the rolls of which may
be operated at the same or at different peripheral
speeds. The composition may be passed repeatedly
through the nip between the rolls of the mill, which nip
may be progressively decreased in size. The nip between
the rolls of the mill may be decreased to a size as low
as 0.1 mm with the result that very high shear may be
applied to the composition which assists in breaking
down aggregates of particulate silicon carbide which may
be present in the composition. On the other hand, where
the composition is of relatively low viscosity and has
more mobile consistency it may be mixed by rapid
stirring with a bladed mixer.
The composition may be converted into a fibre by
any suitable spinning process. The spinning process may
be, for example, a wet spinning process in which a fibre
is formed by extruding the composition through a
suitably sized orifice and into a liquid medium which is
a non-solvent for the organic polymeric material, or a
fibre may be drawn from the composition. Such spinning
processes are more suitable for use with compositions
containing relatively low proportions of a silicon
carbide. Alternatively, the spinning process may be a
dry spinning process in which the composition is
extruded through a suitably sized orifice and the liquid
medium is removed from the fibre by evaporation, eg by
heating the fibre to evaporate the liquid medium. Such
a spinning process is generally more suitable for use
with compositions containing relatively high proportions
of silicon carbide. Where the fibre comprises a sheath
Z~Q~
of silicon carbide on a core of another material the
fibre may be produced by co-extrusion of the core and
the composition.
The fibre which is produced comprises silicon
carbide particles in a matrix of organic polymeric
material, and in the next stage of the process of the
invention this fibre is heated in order to decompose the
organic polymeric material in the fibre. The fibre is
heated to an elevated temperature at which the organic
polymeric material in the fibre is decomposed. A
suitable temperature will depend to some extent on the
nature of the organic polymeric material, but in general
a temperature of up to 500C will suffice. This heating
may generally be effected in an oxygen-containing
atmosphere, eg in air, as the presence of such an
atmosphere assists in the decomposition of the organic
polymeric material. Alternatively, the heating may be
effected in an inert atmosphere, eg in nitrogen or
argon, in order to leave a small proportion of carbon in
the fibre which aids the sintering of the silicon
carbide particles in a subsequent stage of the process.
In a subsequent stage of the process the fibre is
further heated in order to sinter the particles of
silicon carbide. The temperature which is required in
order to effect this sintering will generally be above
1000C and may be as high as 1500C or even greater, eg
up to about 2000C. Sintering may be aided by including
in the composition a small proportion of a sintering aid
for example a known sintering aid such such as boron or
carbon. Sintering at elevated temperature assists in
achieving a high degree of crystallinity in the fibre of
the invention and a high degree of crystallite size
size stability.
The later heating stage of the process of the
invention will generally be effected in an inert
2~C~Z,~
- 15 -
atmosphere by which we mean in an atmosphere which is
unreactive with the silicon carbide at the temperature
of heating. A suitable inert atmosphere is that of an
inert gas, eg helium or argon, or a vacuum. The entire
heating stage is not necessarily effected in an
atmosphere of an inert gas or in a vacuum. For example,
as stated above, in the initial heating stage in which
the organic polymeric material is removed from the fibre
it is advantageous to effect the heating in an
oxygen-containing atmosphere, eg in air, as the presence
of oxygen assists in decomposition of the organic
polymeric material by burning. However, in the later
heating stage of the process in which the silicon
carhide particles are sintered at a temperature above
that at which the organic polymeric material is
decomposed, the presence of an atmosphere containing
oxygen should be avoided as the oxygen may react with
the silicon carbide to produce silica. It may also be
necessary to avoid the use of nitrogen as nitrogen may
react with the silicon carbide to produce silicon
nitride.
The final heating stage in which the particles of-
silicon carbide in the fibre are sintered may be
effected for a time sufficient for the density of the
fibres to be increased to a value approaching the
maximum density, eg to a density of at least 95%,
preferably at least 98%, of the density of silicon
carbide per se.
The silicon carbide fibres of the invention may
have any suitabile diameter, and the orifice through
which the composition is spun or extruded in the process
of the invention, or the speed at which a fibre is
drawn, will be chosen to result in the production of a
silicon carbide fibre having the desired diameter. The
diameter of the silicon carbide fibre may be, for
z~
- 16 -
example, less than 500 microns, or less than 100 microns
or 50 microns as fibres having such diameters are
generally used in the reinforcement applications
hereinbefore referred to. The diameter of the silicon
carbide fibre may be as low as 1 micron or more usually
10 microns. ~owever, the fibre diameters hereinbefore
referred to are merely by way of illustration and are
not intended to be limiting.
The invention is illustrated by the following
examples in which all parts are expressed in parts by
weight.
EXAMPLE 1
A composition of 49.5 parts of silicon carbide
powder having a particle size in the range 0.1 micron to
2 microns and comprising > 98% by weight of silicon
carbide, 0.5 part of boron powder as a sintering aid,
4.5 parts of hydrolysed polyvinyl acetate having a
degree of hydrolysis of 80%, and 9 parts of water was
mixed on twin-roll mill operating at 22C and formed
into a band on the mill. The band was removed from and
recharged to the mill in order to form a homogeneous
mixture of the components in the composition. The
composition was then charged to a screw extruder and
extruded at a temperature of 22C through a 300 micron
diameter orifice into air and the resultant fibre was
dried by heating in an oven at 80C. The dried fibre was
heated in an oven in an atmosphere of argon at a rate of
increase of temperature of 1C per minute up to 800C
and heated at 800C for 1 hour in order to decompose the
organic polymeric material from the fibre. Analysis of
the fibre indicated that it contained about 1% by weight
of residual carbon which was useful as a sintering aid.
The fibre was then heated for half an hour at 2040C in
an oven under an argon atmosphere in order to sinter the
particles of silicon carbide in the fibre and in order
2~QC~2~
- 17 -
to densify the fibre. The fibre was then allowed to
cool in an atmosphere of argon.
Chemical analysis of the silicon carbide fibre
indicated a carbon content of 31.6 weight % compared
with a theoretical value of 30.4 weight %, allowing for
the boron present as a sintering aid. The fibre which
was produced thus consisted substantially of silicon
carbide, and in particular substantially in excess of
90% by weight of silicon carbide.
Chemical analysis for oxygen, boron and nitrogen
indicated that these elements were present in
percentages by weight of 0.1% < 0.1% and
0.34% respectively.
By way of comparison chemical analysis of a
commercially produced silicon carbide fibre produced
by thermal decomposition of an organosilicon polymer
fibre ('Nicalon', Nippon Carbon Co.) showed that the
fibre contained 13.1% by weight of oxygen, corresponding
to 24.6% by weight of silica, and chemical analysis of
another commercially produced silicon carbide fibre
produced by thermal decomposition of a titanocarbosilane
polymer fibre ('Tyranno', Ube Industries Ltd) showed
that the fibre contained 13.0% by weight of oxygen,
corresponding to 24.4% weight of silica.
A sample of the silicon carbide fibre produced as
described in this example was mounted in a block of
acrylic resin and the block was polished to reveal a
flat smooth section through the fibre and transverse to
the length of the fibre. The section of the fibre was
then examined by energy dispersive X-ray analysis and
line scans for Si and C were carried out. No part of the
section transverse to the length of the fibre contained
an area greater than 5 micron in dimension over which
the count of Si X-rays was then half that in the bulk
of the silicon carbide, thus indicating that the silicon
2~ Z~I
- 18 -
carbide fibre was substantially homogeneous across a
transverse section of the fibre.
By way of comparison a commercially produced
silicon carbide fibre produced by chemical vapour
disposition onto a tungsten filament ('Sigma', Sigma
Composites Ltd) was similarly mounted in block of
acrylic resin, polished, and examined by energy
dispersive x-ray analysis. The analysis indicated a
region of dimension approximately 12 micron in the
centre of the fibre which did not contain silicon
carbide and which consisted of tungsten, thus indicating
that the fibre was not substantially homogeneous across
a transverse section of the fibre.
The change in crystal structure, and specifically
the change in crystallite size, of a silicon carbide
fibre produced as described in this example when heated
to elevated temperature was determined by X-ray
examination. Mean crystallite size, L, was determined
from the width of a given X-ray peak using the formula
L = K A
B cos 0
where A is the wavelength of the radiation used, in this
case Cu K~, and K is the Scherrer constant. In this
case the <111> planes were examined corresponding to a
lattice spacing of 2.51 A and 0, the Bragg angle, was
35.74, and a Scherrer constant K of 1.0 was assumed. B
is the full width of the reflection at half height
corrected for any instrument broadening using the
formula B =~ -/b2~where ~ is the full width at half
~/
height obtained from the sample and b is the full width
at half height of a standard. The standard used was
quartz (Arkansas stone). The peak measured was the 251A
peak or that nearest to 251A.
25~
-- 19 --
A silicon carbide fibre produced as described in
this example was subjected to the X-ray examination
described above, both prior to and after heating to
1500C in an atmosphere of argon for 10 hours. Both
prior to ànd after heating the apparent size of the
crystallites in the silicon carbide fibre was >1000 A
indicating that there was no change in the crystalline
microstructure of the silicon carbide even after heating
to 1500C.
By way of comparison, a 'Nicalon' silicon carbide
fibre and a 'Sigma' silicon carbide fibre as referred to
above were subjected to the X-ray examination as
described in this example, both prior to and after
heating in an atmosphere of argon at 1500C for 10
hours. In the case of the 'Nicalon' fibre the apparent
crystallite size in the fibre increased on heating from
50 A to 150 A, and in the case of the 'Sigma' fibre the
apparent crystallite size increased from 150 A to
400A, indicating crystalline microstructural instability
in the fibres on heating.
In order to show that prolonged exposure to
elevated temperature of the silicon carbide produced as
described in this example has little if any effect on
the strength of the fibre samples of fibre were heated
at 1500C in air for times ranging up to 100 hours. The
bending strengths of the fibres were then measured on a
3-point bend test at room temperature, with the
following results.
Time of heating Bending Strength
30hours MPa
0 1431
1 1665
1437
100 1524
2~C~2;~
- 20 -
EXAMPLES 2 to 6
The procedure of Example 1 above was repeated in
five separate examples to produce silicon carbide fibres
except that the diameter of the orifice of the extruder
was, respectively, 100, 150, 200, 50 and 25 microns.
Chemical analysis indicated that the fibres
consisted substantially of silicon carbide, and X-ray
analysis indicated that the fibres were substantially
homogeneous over a transverse section of the fibres.
EXAMPLES 7 to 9
The procedure of Example 1 above was repeated in
three separate examples to produce silicon carbide
fibres, except that the compositions from which the
fibres were produced comprised respectively,
49.5 parts of silicon carbide powder, 3 parts of
hydrolysed polyvinyl acetate, 2 parts of glycerol, and 9
parts of water,
49.5 parts of silicon carbide powder, 1 part of
hydrolysed poly vinyl acetate, 2 parts of glycerol, and
9 parts of water, and
49.5 parts of silicon carbide powder, 1 part of
hydrolysed polyvinyl acetate, 2 parts of glycerol,
and 10 parts of water, and the orifice of the extruder
had a diameter of 100 microns.
Chemical analysis indicated that the fibres
consisted substantially of silicon carbide, and X-ray
analysis indicated that the fibres were substantially
homogeneous over a transverse section of the fibres.
EXAMPLE 10
-
The procedure of Example 1 was repeated except
that the composition from which the fi~res were produced
comprised 50 parts of silicon carbide powder containing
0.5% of boron, 10 parts of polyvinyl butyrol, and 12
parts of cyclohexanone, and the composition was extruded
through orifices of diameters 300, 100 and 50 microns.
Z~ 22~
- 21 -
Chemical analysis indicated that the fibres
consisted substantially of silicon carbide, and X-ray
analysis indicated that the fibres were substantially
homogeneous over a transverse section of the fibres.
EXAMPLE 11
The procedure of Example 1 was repeated except
that a gel was formed by mixing 20 parts of
polyacrylamide having a molecular weight in the range 5
to 6 x 106 with 80 parts of water and the mixture was
allowed to stand for 4 days, the composition from which
the fibres were produced comprised 50 parts of silicon
carbide containing 0.5 part of boron, and 15 parts of
the gel produced as described above, and the composition
was extruded through orifices of diameters 300, 100 and
50 microns.
Chemical analysis indicated that the fibres
consisted substantially of silicon carbide, and X-ray
analysis indicated that the fibres were substantially
homogeneous over a transverse section of the fibres.
Fibres of diameter 100 microns which after
sintering had a density of 99.8% of the theoretical
maximum density were heated in air at 1500C for 100
hours. The bending strength of the fibres so heated,
determined at room temperature, was 1197 MPa, with a
standard deviation of 204 MPa. Fibres which had not
been so heated in air had a bending strength of 1314 MPa
with a standard deviation of 193 MPa.
EXAMPLE 12
The procedure of Example 1 was repeated except
that a gel was formed by mixing 20 parts of
hydroxypropyl methyl cellulose and 100 parts of water,
and the mixture was allowed to stand for 4 days, the
composition from which the fibres were produced
comprised 50 parts of silicon carbide containing 0.5% of
boron and 20 parts of the gel produced as described
2~ 2~L
- 22 -
above, and the composition was extruded through orifices
of diameters 300, 100 and 50 microns.
Chemical analysis indicated that the fibres
consisted substantially of silicon carbide, and X-ray
analysis indicated that the fibres were substantially
homogeneous over a transverse section of the fibres.
EXAMPLE 13
The procedure of Example 1 was repeated except
that the silicon carbide which was used was in the form
of a powder produced by a plasma process and having a
surface area of 23 m2 g~1~ the composition comprised 69
parts of silicon carbide, 1 part of boron powder, 3
parts of partialy hydrolysed polyvinyl acetate, 4.5
parts of D-glucose (as a source of carbon which is an
aid to sintering),2 parts of glycerol, and 9 parts of
water, and the composition was extruded through orifices
of diameters 50, 100 and 200 microns. The silicon
carbide fibres, after sintering, had a density of 98.4%
of the theoretical density.
Chemical analysis indicated that the fibres
consisted substantially of silicon carbide, and X-ray
analysis indicated that the fibres were substantially
homogeneous over a transverse section of the fibres.
Fibres of diameter 100 microns were heated in air
at 1500~C for 100 hours. The bending strength of the
fibres so heated, determined at room temperature, was
1139 MPa, with a standard deviation of 143 MPa. Fibres
which have not been so heated in air had a bending
strength of 1193 MPa with a standard deviation of 188
MPa.
EXAMPLE 14
The procedure of Example 1 was repeated except
that the silicon carbide powder which was used comprised
95 weight% ~-SiC and 5 weight % ~-SiC and had a surface
area of 19 m2 g-~, the compositition comprised 49 parts
2~ 2~
- 23 -
of silicon carbide, 1 part of boron, 4.5 parts of
partially hydrolysed polyvinyl acetate, 2 parts of
glycerol and 10 parts of water, and the composition was
extruded through orifices of diameters 100 and 200
S mirons.
Chemical analysis indicated that the fibres
consisted substantially of silicon carbide, and X-ray
analysis indicated that the fibres were substantially
homogeneous over a transverse section of the fibres.
Example 15
The procedure of ~xample 1 was repeated except
that the silicon carbide which was used consisted of
hexagonal silicon carbide having a surface area of
15 m2g-1, the composition comprised 49 parts of silicon
carbide, 1 part of boron powder, 4.5 parts of partially
hydrolysed polyvinyl acetate, 4.5 parts of D-glucose (as
a source of carbon which is an aid to sintering),
2 parts of glycerol, and 10 parts of water, and the
composition was extruded through an orifice of
diameter 200 microns.
Chemical analysis indicated that the fibres
consisted substantially of silicon carbide, and X-ray
analysis indicated that the fibres were substantially
homogeneous over a transverse section of the fibres.
The fibres were heated in air at 1500C for
100 hours. The bending strength of the fibres so heated,
determined at room temperature, was 1656 MPa, with a
standard deviation of 191 MPa. Fibres which have not
been so heated in air had a bending strength of 1622 MPa
with a standard deviation of 224 MPa.
